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Optimum Control of Flight Vehicle Under the Conditions of Uncertainty,
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Technical Report
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Accession Number:
ADA007400
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Abstract:
No Abstract Identified
Author(s):
Zhelnin, Yu. N.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Working copy machine trans. of Tsentralnyi Aerogidrodinamicheskii Institut. Uchenye Zapiski (USSR) v2 n2 p50-57 1971.
Annotation:
Optimum Control of Flight Vehicle Under the Conditions of Uncertainty--Translation.
Pagination:
0026
Security Markings
DOCUMENT & CONTEXTUAL SUMMARY
Distribution:
Approved For Public Release
RECORD
Collection:
TR
Identifying Numbers
Report Number(s):
FTD-MT-24-0345-75
Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*ATMOSPHERE ENTRY
,
*HYPERSONIC VEHICLES
,
USSR
,
OPTIMIZATION
,
BOUNDARY VALUE PROBLEMS
,
PERTURBATIONS
,
TRANSLATIONS
,
TRAJECTORIES
Field(s)/Group(s):
Guided Missile Trajectories, Accuracy and Ballistics
Report Date:
1975 Feb 13